N187SW, cancelled Sep 12, 2005

Service difficulty reports · 90

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N187SW' AND deregistration_id = 'N187SW-2005-09-12'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA200514909Selector · malfunctionedCREW REPORTED FLAP CONTROL FAULT AND ADVANCED SWS WHEN FLAPS SELECTED. REMOVED AND REPLACED FLAP LEVER IAW MM 27-50-01, OPERATIONAL CHECK GOOD.Apr 15, 2005 · N187SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200514858Selector · bindingFLAP SELECTOR BINDS IN 45 DEG NOTCH. REPLACED FLAP SELECTOR LEVER ASSY IAW EMB MM 27-50-01, OPERATIONAL CHECK GOOD.Apr 9, 2005 · N187SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200514857Actuator · malfunctionedONCE AIRBORNE, RIGHT RUDDER WOULD ONLY MOVE HALF WAY. REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW EMB MM 27-22-02 , OPERATIONAL CHECK IAW EMB MM 27-24-00 GOOD.Apr 9, 2005 · N187SW · Emb EMB120ER · Rudder Control SystemSDR SWIA200514415Fcu · malfunctionedAFTER LANDING FLAPS STAYED AT 45 DEGREES. INSTALLED A SERVICEABLE FCU. OPERATIONAL CHECK GOOD.Jan 17, 2005 · N187SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200514339Actuator · malfunctionedON TAKEOFF, THE RIGHT RUDDER HAD VERY LIMITED TRAVEL. REPLACED GREEN HYDRAULIC RUDDER ACTUATOR IAW 27-22-02. OPS AND LEAK CHECK GOOD.Jan 6, 2005 · N187SW · Emb EMB120ER · Rudder ActuatorSDR SWIA200413590Control Panel · malfunctionedSTALL WARNING ON MAP WILL NOT CLEAR. REMOVED AND REPLACED STALL WARNING PANEL. OPERATIONAL CHECK GOOD. P/N: 120-84428-505, S/N OFF: 1200034R.Jul 15, 2004 · N187SW · Emb EMB120ER · Stall Warning SystemSDR SWIA200413524Bracket · crackedLEFT WING UPPER 2ND FROM LAST SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. SKIN SUPPORT REMOVED AND REPLACED IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413523Bracket · crackedLEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET IS CRACKED AT RIB 22. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP IAW SRM 57-20-07, 51-40-05, 51-25-00, 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413495Rib · wornRIGHT WING LEADING EDGE INBOARD OF NACELLE, OUTBOARD ATTACH POINT RIB WORN THROUGH. DISCOVERED DURING C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1.May 6, 2004 · N187SW · Emb EMB120ER · Wing, Rib/BulkheadSDR SWIA200413494Support Bracket · crackedRIGHT WING UPPER 4TH FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-40, 51-40-05, AND 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413493Rib · crackedRIGHT WING FORWARD RIB 19 CRACKED AT TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 19 REPLACED IAW EMB 120 SRM 51-40-07, 51-40-04, 51-40-05, 51-22-00, AND 51-40-07, AND CONTINUATION SHEET 1 AND 2.May 6, 2004 · N187SW · Emb EMB120ER · Wing, Rib/BulkheadSDR SWIA200413492Rib · crackedRIGHT WING FORWARD RIB 20 CRACKED AT TOP TWO SPOTS. DISCOVERED DURING C-CHECK INSPECTION. RIGHT WING FORWARD RIB 20 REPLACED IAW 51-25-00, 51-40-05, 51-40-02, 51-22-00.May 6, 2004 · N187SW · Emb EMB120ER · Wing, Rib/BulkheadSDR SWIA200413491Support Bracket · corrodedRIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET AT RIB 20 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413490Support Bracket · crackedRIGHT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413489Support Bracket · crackedRIGHT WING UPPER FORWARD SKIN SUPPORT BRACKET CRACKED AT RIB 21. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413488Support Bracket · crackedRIGHT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413487Support Bracket · crackedRIGHT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET AT RIB 23 IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLIP IAW SRM 57-20-07, 51-25-00, 52-40-05, 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413486Support Bracket · crackedRIGHT WING RIB 24 LOWER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED CRACKED BRACKET IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413485Structure · crackedLEFT ZONE 193 LOWER FLANGE WING TO FUSELAGE IS CRACKED IN THREE LOCATIONS. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ANGLE IAW EMB 120 SRM 53-20-13 PG 205-206 FIG 202.May 6, 2004 · N187SW · Emb EMB120ER · Wing, Fuselage Attach FittingsSDR SWIA200413484Support Bracket · crackedLEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIPS IAW SRM 57-20-07, 51-40-05, 52-25-00, 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413483Support Bracket · crackedLEFT WING UPPER 3RD FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413482Support Bracket · crackedLEFT WING UPPER 2ND FROM FRONT SKIN SUPPORT BRACKET CRACKED AT RIB 8. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED SKIN SUPPORT IAW SRM 57-20-07, 51-40-05, 51-25-00, AND 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413481Support Bracket · crackedLEFT WING UPPER AFT SKIN SUPPORT BRACKET CRACKED AT RIB 23. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED SKIN SUPPORT CLAMP IAW SRM 57-20-07, 51-25-00, 51-40-05, AND 51-40-02.May 6, 2004 · N187SW · Emb EMB120ER · Wing Miscellaneous StructureSDR SWIA200413480Frame · crackedFRAME 15 IN BELLY CRACKED FRAME AT AFT AIR STAIR ACTUATOR. DISCOVERED DURING C-CHECK INSPECTION. FRAME REPAIRED IAW EMB 120 SRM 53-00-04 PG 201-204.May 6, 2004 · N187SW · Emb EMB120ER · Fuselage Main, FrameSDR SWIA200412932Proximity Switch · faultyFIRST FLIGHT AURAL WARNING TRIM CHECK FAILS. REMOVED LEFT AND RIGHT ELEVATOR TRIM PROX SWITCHES HAND SHAKE CONNECTORS AND REPLACED WITH ENVIRONMENTAL SPLICE CONNECTORS IAW EMB 120 WMM 20-21-00 AND 31-52-00, OPS CHECKED GOOD.Feb 20, 2004 · N187SW · Emb EMB120ER · Elevator Control SystemSDR SWIA200412861Shutoff Valve · malfunctionedSMOKE IN COCKPIT AND CABIN WITH BOTH PACKS OFF. REMOVED AND REPLACED LT ENGINE PRESSURE REGULATOR SHUT OFF VALVE WITH SERVICEABLE UNIT IAW MM 36-10-04. OPS CHECKS GOOD AT THIS TIME.Feb 5, 2004 · N187SW · Emb EMB120ER · Pneumatic Distribution SystemSDR SWIA200412853Annunciator · malfunctionedFLAP CONTROL FAULT, DISAGREE, AND ASYM MESSAGE OVERHEAD FLAP AND ADVANCED SWS ON MAP STAY ON. INSTALLED A SERVICEABLE FLAP ANNUNCIATOR IAW 27-50-05. OPS CHECK GOOD. REMOVED AND REPLACED FLAP CONTROL UNIT. P/N OFF: 347200-1001, SN OFF: 0194.Jan 27, 2004 · N187SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200312609Light · shortedEMERGENCY EXIT LIGHTS AT 6A AND 6C OVERWING EXIT AND THE MIDDLE CEILING LIGHT AS WELL AS FOUR OR FIVE FLOOR LEVEL LIGHTS DO NOT ILLUMINATE OR JUST BARELY LIGHT UP. FOUND SHORT AT LEFT OVERWING EMERGENCY EXIT FLOOD LIGHT. RECONNECTED, REPOSITIONED TERMINALS ANov 13, 2003 · N187SW · Emb EMB120ER · Emergency LightingSDR SWIA200312408Control Unit · malfunctionedCONTROL FAULT WITH FLAP AND ADVANCED SWS IN FLIGHT INBOARD FLAPS FLASHING. CLEARED WITH RESET IAW QRH. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR AND REPLACED FCU IAW 27-80-08. OPS AND LEAK CHECKS GOOD. PN: 320300-1005 SN OFF: 0885Sep 14, 2003 · N187SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200312381Control Unit · malfunctionedON APPROACH INTO SLC WE SELECTED FLAPS 15 AND GOT THE ''CONTROL FAULT'' WITH THE ''FLAP'' AND ''ADVANCED SWS'' ON THE MAP. QRH PROCEDURE CORRECTED PROBLEM.REMOVED AND REPLACED FLAP CONTROL UNIT IAW MM 27-50-06. OPS CHECK GOOD.Sep 6, 2003 · N187SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200312382Bracket · crackedRT INBOARD FLAP ROLLER BRACKET IS CRACKED. REPLACED RT INBOARD FLAP OUTBOARD GAP PANEL ROLLER BRACKET. CHECKS GOOD.Sep 2, 2003 · N187SW · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200312076Wire Harness · unserviceableWHEN LANDING GEAR LEVER WAS MOVED DOWN, RIGHT RED TRANSITION -A- LIGHT STAYED ON, RIGHT GREEN -A- LIGHT DID NOT COME ON. REMOVED AND INSTALLED SERVICEABLE WIRE HARNESS. OPS CHECK GOOD ON GEAR SWING IAW EMB MM 32-61-01. P/N OFF/ON 120-22623-501.Jun 7, 2003 · N187SW · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200312070Actuator · malfunctionedINFLIGHT FLAP CONTROL FAULT INDICATION WOULD NOT CLEAR. RETURNED TO FIELD. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPS AND LEAK CHECKS GOOD IAW MM 27-50-09.Jun 4, 2003 · N187SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200311896Relay · malfunctionedDURING FLIGHT, RIGHT MAIN ''A'' GREEN LIGHT ILLUMINATED. GEAR WOULD NOT EXTEND - ALL THREE GEAR RED LIGHTS ILLUMINATED EXCEPT RIGHT ''A'' RED WITH HANDLE DOWN. AFTER 5 MINUTES THE PROBLEM FIXED ITSELF AND THE GEAR LOWERED NORMALLY. REPLACED LANDING GEAR RELApr 21, 2003 · N187SW · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR SWIA200311687Connector · contaminatedCONTROL FAULT ON INBOARD FLAPS DURING FLAP RETRACTION. CLEANED CONNECTOR ON FLAP INBOARD ACTUATORS ON BOTH SIDES. RAN SEVERAL TIMES. NO FAULTS AT THIS TIME.Jan 7, 2003 · N187SW · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200211584Wire Harness · malfunctionedON TAKEOFF FROM PSP, THE RT GEAR GREEN SYS A LIGHT REMAINED ON. UPON PUTTING GEAR DOWN AT LAX, THE GEAR DID NOT COME DOWN. PERFORMED ELECTRIC OVERRIDE QRH PROCEDURE AND THE GEAR CAME DOWN OK. REMOVED RIGHT A-HARNESS, REPAIRED AND REINSTALLED IAW 32-60-00. Dec 16, 2002 · N187SW · Emb EMB120ER · Landing Gear System WiringSDR SWIA200211579Annunciator · malfunctionedAFTER LANDING AT PSP THE INBOARD FLAPS WOULD NOT RETRACT. REPLACED FLAP ANNUNCIATOR WITH A SERVICEABLE UNIT. OPS CHECK GOOD.Dec 15, 2002 · N187SW · Emb EMB120ER · Trailing Flap Position Indicating SystemSDR SWIA200211561Switch · lack of lubeFORWARD DOOR LIGHT ILLUMINATED INFLIGHT. LUBED FORWARD DOOR MICROSWITCHES. OPS CHECK GOOD.Dec 1, 2002 · N187SW · Emb EMB120ER · Door Warning SystemSDR SWIA200211185Wire · brokenFLOOR LIGHTING IN FRONT OF GALLEY NOT WORKING. REPAIRED BROKEN WIRE. OPS CHECK GOOD.Aug 30, 2002 · N187SW · Emb EMB120ER · Light System WiringSDR SWIA200210925Link · corrodedPASSENGER DOOR PUSH-PULL LINKS CORRODED (FORWARD AND AFT). REMOVED AND REPLACED PASSENGER DOOR FORWARD AND AFT PUSH-PULL LINKS IAW EMB MM 52-11-03.May 9, 2002 · N187SW · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200210924Wire · burnedWIRE AT CANNON PLUG J0958 PIN F ON RIGHT SIDE DC RELAY BOX IS BURNED AND NEEDS TO BE REPLACED. REMOVED AND REPLACED WIRE W208-0064 AT CANNON PLUG J0958 PIN F WITH A NEW WIRE 1 GAUGE LARGER AND PERFORMED OPERATIONAL CHECK AS PER MM 30-40-00. OPS CHECK GOOD.May 9, 2002 · N187SW · Emb EMB120ER · Electrical Power System WiringSDR SWIA200210923Torque Tube · corrodedNR 2 AND NR 3 PASSENGER DOOR STEP RODS FOUND CORRODED DURING INSPECTION. REMOVED AND REPLACED NR 2 AND NR 3 PASSENGER DOOR STEP TORQUE TUBES IAW EMB MM 52-10-03.May 9, 2002 · N187SW · Emb EMB120ER · Entrance StairsSDR SWIA200210922Actuator · corrodedPASSENGER DOOR STEP ACTUATOR ARM FOUND CORRODED. REMOVED AND REPLACED PASSENGER DOOR STEP ACTUATOR ARM WITH NEW. OPS CHECK GOOD.May 9, 2002 · N187SW · Emb EMB120ER · Entrance StairsSDR SWIA200210830Pcu · malfunctionedON TAKEOFF, COULD NOT MOVE RUDDER PAST HALF TRAVEL TO THE RIGHT. TURNING BLUE SYSTEM OFF MADE NO DIFFERENCE. UPON LANDING FULL TRAVEL WAS RESTORED. REPLACED RUDDER PCU. INFLIGHT FUNCTIONAL TEST OF RUDDER SYSTEM NORMAL. FLIGHT TEST OK.Apr 28, 2002 · N187SW · Emb EMB120ER · Rudder Control SystemSDR SWIA200210704Support · wornTHE ELEVATOR TRIM FORWARD QUADRANT IDLER SPROCKET SUPPORT HAS CHAIN TRACKS WORN IN IT. REMOVED DAMAGED SUPPORT AND INSTALLED NEW IAW EMB SRM 51-40-02.Mar 2, 2002 · N187SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200210618Trim Tab · out of adjustON DESCENT INTO EKO, TRIM FAIL WARNING WENT OFF. AFTER A/P DISCONNECT, AIRCRAFT PITCHED UP AT 230 KTS WITH ELEVATOR TRIM AT FULL NOSE DOWN STOP. AIRCRAFT NOT UNDER NORMAL CONTROL UNTIL SLOWED BELOW 200 KTS. ADJUSTED RT ELEVATOR TRIM TAB AS REQUIRED TO RECEIFeb 1, 2002 · N187SW · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200210588Controller · failedON DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE AT ALL. MANUAL CONTROLLER WOULD NOT FUNCTION. RETURNED TO ELKO. REMOVED AND REPLACED AUTO PRESSURIZATION CONTROLLER IAW EMB MM 21-30-01. AUTO PRESSURIZATION OPS CHECKS GOOD IAW EMB MM 21-30-00.Jan 25, 2002 · N187SW · Emb EMB120ER · Cabin Pressure ControllerSDR SWIA200110514Stringer · crackedSTRINGER NR 8 CRACKED AT LEFT WING NR 2 FUEL PANEL. REPAIRED STRINGER CRACK IAW EMB SRM 57-20-03.Dec 28, 2001 · N187SW · Emb EMB120ER · Wing, Longeron/StringerSDR SWIA200110031Warning System · activatedAUTO FEATHER WARNING ON TAKE OFF ROLL.RAN BOTH ENGINES W/AUTO FEATHER ARMED. APPLIED 60% TORQUE. NO AUTO FEATHER WARNINGS. OPS CHECK GOOD.Jul 11, 2001 · N187SW · Emb EMB120ER · Propeller Feathering/ReversingSDR SWIA972561Valve · failedRIGHT PACK FAILED DURING CLIMB. APPROXIMATELY 1 MINUTE LATER, THE LAV SMOKE DETECTOR STARTED BEEPING AND THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. WITH RECIRCS AND GASPERS OFF, THE CABIN SLOWLY CLEARED. REMOVED LEFT AND RIGHT RAM AIR VENTILATION VALMay 9, 2001 · N187SW · Emb EMB120ER · Cabin Cooling System
Back to N187SW, cancelled Sep 12, 2005